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Feasibility Studies for VTOL UAVAutonomous Operations with the Possibility of Ship board Auto Recovery using Simulation Techniques

机译:VTOL无人机自主运行的可行性研究,可通过仿真技术实现船上自动恢复

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The purpose of this Office of Naval Research sponsored Future Naval Capabilities UAV project is to demonstrate the feasibility to automatically signal the initiation of UAV descent. The objective is to recover the UAV on-board a moving vessel within reasonable safety margins regardless of the seaway. The Energy Index, the operative component of the Landing Period Designator, identifies quiescent periods to initiate aircraft descent based on aircraft deck limit definitions. Dynamic Interface simulation provides the physical information from which initial deck limits might be derived. Energy Index quiescent indications for UAV recovery opportunities are presented outside of current operating limits. A brief synopsis of the theory and calculation of the ship motion simulation and Energy Index programs, are discussed. The use of flight simulator to forecast physical deck motion and deck motion limits, is discussed. UAV flight test programs using simulation, are described. Undercarriage deflection to encountered deck forces and aircraft stability, were calculated. Using Launch and Recovery "rondelles", the deck limits at specific ship's speeds may be identified. Impacts on the proposed deck limits, are discussed. Percent improvement of operational availability is demonstrated.The results using simulated data are compared to those recorded during dynamic interface testing. Good correlation is shown between the deck limits calculated by simulation with that recorded at sea. The index performed to specification showing no exceptions or failures. System components are presented and a short discussion of the UAV landing profile, is offered.
机译:该海军研究办公室赞助的“未来海军能力”无人机项目的目的是证明自动发出“无人机”下降信号的可行性。目的是在不考虑海路的情况下,在合理的安全裕度范围内,将移动的无人机恢复到船上。能源指数是着陆期间指示符的有效组成部分,它根据飞机甲板限制定义确定休止期,以启动飞机下降。动态接口仿真提供了可以从中得出初始甲板极限的物理信息。无人机恢复机会的能源指数静态指示超出了当前运行限制。讨论了船舶运动仿真和能源指数程序的理论和计算的简要提要。讨论了如何使用飞行模拟器来预测甲板运动和甲板运动极限。描述了使用模拟的无人机飞行测试程序。计算了遇到的甲板力的起落架挠度和飞机稳定性。使用发射和恢复“龙卷风”,可以确定特定船速下的甲板极限。讨论了对提议的甲板限制的影响。证明了业务可用性的百分比提高。 将使用模拟数据的结果与动态接口测试期间记录的结果进行比较。通过模拟计算得出的甲板极限与海上记录的极限之间显示出良好的相关性。对规范执行的索引不显示任何异常或失败。介绍了系统组件,并提供了关于无人机着陆剖面的简短讨论。

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